View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 18113.80554540 -.00000044 00000-0 -62063-5 0 9995
2 24278 98.5221 320.0425 0349339 251.9830 104.2956 13.53083012 70883
Epoch (UTC): | 23 April 2018 19:19:59 |
Eccentricity: | 0.0349339 |
inclination: | 98.5221° |
perigee height: | 801 km |
apogee height: | 1321 km |
right ascension of ascending node: | 320.0425° |
argument of perigee: | 251.9830° |
revolutions per day: | 13.53083012 |
mean anomaly at epoch: | 104.2956° |
orbit number at epoch: | 7088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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